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US4220364A - Flush type latches - Google Patents

Flush type latches Download PDF

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Publication number
US4220364A
US4220364A US05/882,174 US88217478A US4220364A US 4220364 A US4220364 A US 4220364A US 88217478 A US88217478 A US 88217478A US 4220364 A US4220364 A US 4220364A
Authority
US
United States
Prior art keywords
keeper
panel
drive bar
screwthreaded
latch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/882,174
Inventor
L. Richard Poe
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hartwell Corp
Original Assignee
Hartwell Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hartwell Corp filed Critical Hartwell Corp
Priority to US05/882,174 priority Critical patent/US4220364A/en
Application granted granted Critical
Publication of US4220364A publication Critical patent/US4220364A/en
Assigned to MEES PIERSON N.V., NEW YORK AGENCY reassignment MEES PIERSON N.V., NEW YORK AGENCY ASSIGNMENT OF SECURITY INTEREST IN UNITED STATES TRADEMARKS AND PATENTS Assignors: HARTWELL CORPORATION
Assigned to MEESPIERSON CAPITAL CORP., DELAWARE CORPORATION reassignment MEESPIERSON CAPITAL CORP., DELAWARE CORPORATION ASSIGNMENT OF SECURITY INTEREST IN UNITED STATES TRADEMARKS AND PATENTS Assignors: MEES PIERSON, N.V., NEW YORK AGENCY
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05BLOCKS; ACCESSORIES THEREFOR; HANDCUFFS
    • E05B15/00Other details of locks; Parts for engagement by bolts of fastening devices
    • E05B15/02Striking-plates; Keepers; Bolt staples; Escutcheons
    • E05B15/0205Striking-plates, keepers, staples
    • E05B15/024Striking-plates, keepers, staples adjustable
    • E05B15/025Striking-plates, keepers, staples adjustable the striker being movable by a screw/nut
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/08Bolts
    • Y10T292/0911Hooked end
    • Y10T292/0913Sliding and swinging
    • Y10T292/0914Operating means
    • Y10T292/0917Lever
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T292/00Closure fasteners
    • Y10T292/68Keepers
    • Y10T292/705Adjustable

Definitions

  • Aircraft are provided with a substantial number of outwardly exposed flush panels which are removable or hinged to the surrounding surface of the aircraft, such panels having one or more flush mounted latch assemblies. Due to the high forces exerted on the surface of the aircraft, proper adjustment between a hook latch arm of a latch assembly and a corresponding keeper arm secured to an adjacent portion of the aircraft structure is of primary importance. Adjustment requires access to the keeper; usually this has required complete disengagement of the hook arm and keeper.
  • the present invention is directed to a tension adjuster for flush type latches which provides access while the hook arm and keeper element are in mutual engagement to facilitate dependable and predictable loading of the flush type latches to insure dependibility under extreme conditions of use, and is summarized in the following objects:
  • a novelly arranged keeper is longitudinally movable by means of a novelly arranged screw shaft disposed inwardly of but adjacent the surface of the aircraft and is positioned for access by a turning tool readily accessible when the flush latch is in its initial open position.
  • FIG. 1 is a fragmentary sectional view of a panel and frame fitted with a flush type latch assembly and showing in section the tension adjuster for the latch.
  • FIG. 2 is an enlarged sectional view of the tension adjuster taken through 2--2 of FIG. 1.
  • FIG. 3 is a partial sectional, partial end view taken through 3--3 of FIG. 2 and turned 90°.
  • FIG. 4 is a transverse sectional view taken through 4--4 of FIG. 2, also turned 90°.
  • the tension adjuster for flush type latches is intended primarily for aircraft represented fragmentarily by skin structure designated 1. Disposed flush with the skin structure is a panel 2 supported by a frame 3. The panel 2 is provided with a rectangular opening 4, dimensioned to receive a flush type latch assembly 5.
  • the latch assembly 5 may be considered as conventional and includes a handle lever 6 having a pivot pin 7 near one end which permits movement of the handle lever between a flush position and initial angular position and a full open position, the handle being illustrated in its initial angular position.
  • the handle lever 6 is channel shaped in cross section and receives a latch arm 8 connected to the handle lever 6 by a pivot pin 9.
  • the extended ends of the handle lever and latch arm are disposed at one end of the rectangular opening 4 and the extremity of the latch arm 8 is provided with a hook 10.
  • a linking latch 11 capable of manual movement so that the handle lever may be moved to the initial angular position shown and a full angular position not shown.
  • the hook extremity 10 is positioned adjacent one side of the frame 3 and receives a U-shaped keeper 12 comprising a cross portion 13 and parallel portions 14. Secured to the adjacent portion of the frame 3 is a guide block 15 having parallel bores 16 which slidably receive the parallel portions 14 of the keeper 12.
  • the guide block 15 includes a mounting plate 17 which is secured to the frame 3 by screws 18.
  • the extended ends of the parallel portions 14 are joined by a cross bar 19 which is secured thereto by anchor pins 20.
  • a screwthreaded bore 21 Centered with respect to the parallel portions 14 of the keeper is a screwthreaded bore 21.
  • the cross bar 19 is provided with a second screwthreaded bore 22 disposed in coaxial relation to the bore 21.
  • the screwthreaded bores are of opposite pitch and receive a drive shaft 23 having external screwthreads of opposite pitch.
  • One end of the drive shaft 23 is in close relation to the corresponding end of the rectangular opening 4.
  • the entire keeper structure is in close proximity to the surface of the panel 2.
  • the drive shaft 23 is provided with a drive socket 24 of polygonal cross section.
  • the drive socket is so positioned that a polygonally shaped rod wrench 25 may be inserted through the opening 4 when the handle lever is in its initial angular position and manipulated into engagement with the drive socket 24.
  • Such wrench is known commercially as an Allen wrench.
  • the handle lever 6 is raised from its flush position to the initial angular position shown in FIG. 1. This provides access to the drive shaft 23 by means of the Allen wrench 25. In this position of the latch assembly, the latch arm 8 and keeper 12 remain in mutual engagement. The drive shaft 23 is then turned causing the keeper 12 to extend or retract. After a tentative adjustment is made, the Allen wrench is removed and the handle lever closed to test the adjustment. It will be noted that while some manipulation of the latch is required in the course of adjustment, the amount of movement is minimal and quickly accomplished.

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  • Clamps And Clips (AREA)

Abstract

A tension adjuster for flush type latches, such as is used by aircraft, of the type wherein a handle is received in an opening and is pivotable between a flush position and an initial open position while the latch arm remains in hooked engagement with a keeper, the tension adjuster utilizing a screwthreaded member to effect longitudinal adjustment of the keeper and being accessible to a turning tool insertable into the end of the opening when the handle is in its initial open position.

Description

BACKGROUND
Aircraft are provided with a substantial number of outwardly exposed flush panels which are removable or hinged to the surrounding surface of the aircraft, such panels having one or more flush mounted latch assemblies. Due to the high forces exerted on the surface of the aircraft, proper adjustment between a hook latch arm of a latch assembly and a corresponding keeper arm secured to an adjacent portion of the aircraft structure is of primary importance. Adjustment requires access to the keeper; usually this has required complete disengagement of the hook arm and keeper.
SUMMARY
The present invention is directed to a tension adjuster for flush type latches which provides access while the hook arm and keeper element are in mutual engagement to facilitate dependable and predictable loading of the flush type latches to insure dependibility under extreme conditions of use, and is summarized in the following objects:
First, to provide a tension adjuster for flush type latches wherein a novelly arranged keeper is longitudinally movable by means of a novelly arranged screw shaft disposed inwardly of but adjacent the surface of the aircraft and is positioned for access by a turning tool readily accessible when the flush latch is in its initial open position.
Second, to provide a tension adjuster which may be substituted for conventional adjusters without replacement of the flush type latch.
BRIEF DESCRIPTION OF THE FIGURES
FIG. 1 is a fragmentary sectional view of a panel and frame fitted with a flush type latch assembly and showing in section the tension adjuster for the latch.
FIG. 2 is an enlarged sectional view of the tension adjuster taken through 2--2 of FIG. 1.
FIG. 3 is a partial sectional, partial end view taken through 3--3 of FIG. 2 and turned 90°.
FIG. 4 is a transverse sectional view taken through 4--4 of FIG. 2, also turned 90°.
DETAILED DESCRIPTION
The tension adjuster for flush type latches is intended primarily for aircraft represented fragmentarily by skin structure designated 1. Disposed flush with the skin structure is a panel 2 supported by a frame 3. The panel 2 is provided with a rectangular opening 4, dimensioned to receive a flush type latch assembly 5.
The latch assembly 5 may be considered as conventional and includes a handle lever 6 having a pivot pin 7 near one end which permits movement of the handle lever between a flush position and initial angular position and a full open position, the handle being illustrated in its initial angular position. The handle lever 6 is channel shaped in cross section and receives a latch arm 8 connected to the handle lever 6 by a pivot pin 9. The extended ends of the handle lever and latch arm are disposed at one end of the rectangular opening 4 and the extremity of the latch arm 8 is provided with a hook 10. When the handle lever 6 is in its flush position, it is joined to the latch arm 8 by a linking latch 11 capable of manual movement so that the handle lever may be moved to the initial angular position shown and a full angular position not shown.
The structure thus far described may be considered as conventional and may be considered as a modification of the structure shown in U.S. Pat. Nos. 2,712,955 or 3,542,410.
The hook extremity 10 is positioned adjacent one side of the frame 3 and receives a U-shaped keeper 12 comprising a cross portion 13 and parallel portions 14. Secured to the adjacent portion of the frame 3 is a guide block 15 having parallel bores 16 which slidably receive the parallel portions 14 of the keeper 12. The guide block 15 includes a mounting plate 17 which is secured to the frame 3 by screws 18.
The extended ends of the parallel portions 14 are joined by a cross bar 19 which is secured thereto by anchor pins 20. Centered with respect to the parallel portions 14 of the keeper is a screwthreaded bore 21. The cross bar 19 is provided with a second screwthreaded bore 22 disposed in coaxial relation to the bore 21. The screwthreaded bores are of opposite pitch and receive a drive shaft 23 having external screwthreads of opposite pitch. One end of the drive shaft 23 is in close relation to the corresponding end of the rectangular opening 4. Also the entire keeper structure is in close proximity to the surface of the panel 2. The drive shaft 23 is provided with a drive socket 24 of polygonal cross section. The drive socket is so positioned that a polygonally shaped rod wrench 25 may be inserted through the opening 4 when the handle lever is in its initial angular position and manipulated into engagement with the drive socket 24. Such wrench is known commercially as an Allen wrench.
Operation of the tension adjuster for flush type latches is as follows:
Initially the handle lever 6 is raised from its flush position to the initial angular position shown in FIG. 1. This provides access to the drive shaft 23 by means of the Allen wrench 25. In this position of the latch assembly, the latch arm 8 and keeper 12 remain in mutual engagement. The drive shaft 23 is then turned causing the keeper 12 to extend or retract. After a tentative adjustment is made, the Allen wrench is removed and the handle lever closed to test the adjustment. It will be noted that while some manipulation of the latch is required in the course of adjustment, the amount of movement is minimal and quickly accomplished.
Having fully described my invention, it is to be understood that I am not to be limited to the details herein set forth, but that my invention is of the full scope of the appended claims.

Claims (2)

I claim:
1. A tension adjuster for a latch having a handle movable between a position flush with a surrounding panel set in a surface structure and an angular position diverging from said panel wherein the extended end of the handle and corresponding portion of said panel forms an aperture exposing a limited area underlying the panel and exposing a panel frame, the latch also having a hook arm extending into said limited area, the tension adjuster comprising:
a. a keeper engaging the hook arm and continuing therefrom;
b. a mounting body secured to the panel frame and slidably receiving the keeper;
c. a drive bar having a first connection with the housing and a second connection wsith the keeper wherein both connections between the drive bar, keeper and housing are screwthreaded and of opposite pitch whereby rotation in one direction increases tension on the hook arm, while rotation in the opposite direction reduces tension on the hook arm, the screwthreaded connections being of equal pitch whereby the drive bar remains essentially in a fixed position one of the connections being screwthreaded to effect reciprocal movement of the keeper upon rotation of the drive bar; and
d. the drive bar having a turning socket extending into one end for receiving a turning tool inserted through said aperture.
2. A tension adjuster for a latch having a handle movable between a position flush with a surrounding panel set in a surface structure and an angular position diverging from said panel wherein the extended end of the handle and corresponding portion of said panel forms an aperture exposing a limited area underlying the panel and exposing a panel frame, the latch also having a hook arm extending into said limited area, the tension adjuster comprising:
a. a keeper engaging the hook arm and continuing therefrom, the keeper being provided with a pair of parallel keeper shafts;
b. a cross bar extending between and secured to the keeper shafts;
c. a mounting body secured to the panel frame and slidably receiving the keeper the mounting body having a pair of bores receiving the keeper shafts;
d. the mounting body and cross bar have coaxial screwthreaded bores of opposite pitch;
e. a drive bar having a first connection with the housing and a second connection with the keeper and the drive bar having coaxial externally screwthreaded portions also of opposite pitch received in the screwthreaded bores, to effect longitudinal movement of the keeper shafts while maintaining the axis of the drive bar in an essentially fixed position;
f. the drive bar having a turning socket extending into one end for receiving a turning tool inserted through said aperture.
US05/882,174 1978-03-01 1978-03-01 Flush type latches Expired - Lifetime US4220364A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US05/882,174 US4220364A (en) 1978-03-01 1978-03-01 Flush type latches

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/882,174 US4220364A (en) 1978-03-01 1978-03-01 Flush type latches

Publications (1)

Publication Number Publication Date
US4220364A true US4220364A (en) 1980-09-02

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US05/882,174 Expired - Lifetime US4220364A (en) 1978-03-01 1978-03-01 Flush type latches

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Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4509216A (en) * 1982-11-29 1985-04-09 Hoover Universal, Inc. Sofa bed mechanism
USRE31935E (en) * 1978-03-01 1985-07-02 Hartwell Corporation Externally accessible adjuster for flush latches
US4549708A (en) * 1982-08-31 1985-10-29 United Technologies Corporation Cowling latch system
US4691952A (en) * 1986-10-06 1987-09-08 Rexnord Inc. Clutching adjustable keeper mechanism
FR2620181A1 (en) * 1987-09-08 1989-03-10 Rexnord Inc ADJUSTABLE LOCKING MECHANISM WITH ACCESSIBLE EXTERNAL COUPLING
US4852923A (en) * 1987-02-27 1989-08-01 Rexnord Holdings Inc. Vertical access adjustable latching mechanism externally accessible adjustable keeper mechanism
US4877274A (en) * 1987-09-02 1989-10-31 The Hartwell Corporation Trigger lock cam
US4991885A (en) * 1987-09-02 1991-02-12 The Hartwell Corporation Trigger lock cam
US5016931A (en) * 1989-06-20 1991-05-21 The Hartwell Corporation Latching mechanism having a pre-adjusted load
US5234238A (en) * 1991-09-26 1993-08-10 Takigen Manufacturing Co., Ltd. Ratchet type latch assembly
US5595409A (en) * 1994-07-05 1997-01-21 Anderson Corporation Gliding door latch assembly
US5802892A (en) * 1996-05-08 1998-09-08 Metro Industries, Inc. Storage system including multifunction lock assembly utilizing lock latch mechanism and lock latch extension mechanism
US6036238A (en) * 1996-10-30 2000-03-14 The Boeing Company Double stroke over center latch
US6234426B1 (en) * 1998-12-03 2001-05-22 Trw Inc. Modular spacecraft construction requiring no tools for assembly and disassembly
WO2002016717A1 (en) * 2000-08-22 2002-02-28 Huf Hülsbeck & Fürst Gmbh & Co. Kg Distance-variable closing stirrup for rotary-latch locks
US20030205904A1 (en) * 2002-05-03 2003-11-06 Paskonis Almantas K. Encapsulated striker assembly
US6755448B2 (en) 2001-06-20 2004-06-29 Hartwell Corporation Blowout latch
US20050167993A1 (en) * 2002-12-19 2005-08-04 Paskonis Almantas K. Single-piece latch strikers with mechanically locked components
US20050218671A1 (en) * 2004-04-06 2005-10-06 Honda Motor Co., Ltd. Structure for attaching striker, having attachment bracket including base and protruding portion
US20060214431A1 (en) * 2005-03-25 2006-09-28 Helsley Thomas J Latch mechanism
US20070241570A1 (en) * 2006-04-03 2007-10-18 Paskonis Almantas K Latch and latch striker interface improvements
US20100051748A1 (en) * 2008-08-26 2010-03-04 Etling Keith A Flush-mounted latching assembly and method of assembling same
US20110133489A1 (en) * 2009-12-09 2011-06-09 Airbus Operations Sas Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
US20110227350A1 (en) * 2010-03-18 2011-09-22 Thai Do Latch with adjustable handle
CN102971213A (en) * 2010-07-09 2013-03-13 空中客车运营简化股份公司 Method for adjusting the doors of a landing gear bay, and associated door
US9273488B1 (en) * 2013-07-15 2016-03-01 Avibank Manufacturing, Inc. Positive locking keeper
US9376215B2 (en) 2013-01-29 2016-06-28 United Technologies Corporation Cowl with pressure driven latch
US9845708B2 (en) 2013-01-29 2017-12-19 United Technologies Corporation Cowl with rate limited lock
US10240389B2 (en) 2015-09-30 2019-03-26 Arconic Inc. Pressure relief door
US10309126B2 (en) 2016-01-21 2019-06-04 Arconic Inc. Pawl latch
US10337218B2 (en) 2015-07-08 2019-07-02 Arconic Inc. Handle mechanisms
US10378256B2 (en) 2015-10-30 2019-08-13 Arconic Inc. Pressure relief latch
US10435929B2 (en) 2015-08-26 2019-10-08 Arconic Inc. Adjustable pressure relief latch
CN110319325A (en) * 2019-04-03 2019-10-11 广州文冲船厂有限责任公司 A kind of cabinet mounting structure
US10604977B2 (en) 2015-08-04 2020-03-31 Arconic Inc. Pressure relief latch
US10676971B2 (en) 2016-06-13 2020-06-09 Arconic Inc. Rotary latch system
US10760304B2 (en) 2015-09-01 2020-09-01 Howmet Aerospace Inc. Adjustable hook latch
US11041331B2 (en) 2015-04-03 2021-06-22 Howmet Aerospace Inc. Latch having tool recess in trigger
US20220267018A1 (en) * 2021-02-20 2022-08-25 Andres Hernandez High visibility hook latch

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1119321A (en) * 1914-06-01 1914-12-01 Frederick Schmidgall Lock-keeper.
US1250574A (en) * 1916-12-26 1917-12-18 Hunt Helm Ferris & Co Fastener for doors.
FR543914A (en) * 1921-11-25 1922-09-12 Adjustable strike
US2089163A (en) * 1933-10-04 1937-08-03 Keil Francis & Son Inc Striker or keeper for locks
US2710214A (en) * 1952-12-31 1955-06-07 Camloc Fastener Corp Latch fastener
US2712955A (en) * 1952-09-15 1955-07-12 Clark Hartwell Draw-in type flush latch
US3664696A (en) * 1971-01-15 1972-05-23 Hartwell Corp Latch adjuster

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1119321A (en) * 1914-06-01 1914-12-01 Frederick Schmidgall Lock-keeper.
US1250574A (en) * 1916-12-26 1917-12-18 Hunt Helm Ferris & Co Fastener for doors.
FR543914A (en) * 1921-11-25 1922-09-12 Adjustable strike
US2089163A (en) * 1933-10-04 1937-08-03 Keil Francis & Son Inc Striker or keeper for locks
US2712955A (en) * 1952-09-15 1955-07-12 Clark Hartwell Draw-in type flush latch
US2710214A (en) * 1952-12-31 1955-06-07 Camloc Fastener Corp Latch fastener
US3664696A (en) * 1971-01-15 1972-05-23 Hartwell Corp Latch adjuster

Cited By (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE31935E (en) * 1978-03-01 1985-07-02 Hartwell Corporation Externally accessible adjuster for flush latches
US4549708A (en) * 1982-08-31 1985-10-29 United Technologies Corporation Cowling latch system
US4509216A (en) * 1982-11-29 1985-04-09 Hoover Universal, Inc. Sofa bed mechanism
US4691952A (en) * 1986-10-06 1987-09-08 Rexnord Inc. Clutching adjustable keeper mechanism
US4852923A (en) * 1987-02-27 1989-08-01 Rexnord Holdings Inc. Vertical access adjustable latching mechanism externally accessible adjustable keeper mechanism
US4877274A (en) * 1987-09-02 1989-10-31 The Hartwell Corporation Trigger lock cam
US4991885A (en) * 1987-09-02 1991-02-12 The Hartwell Corporation Trigger lock cam
FR2620181A1 (en) * 1987-09-08 1989-03-10 Rexnord Inc ADJUSTABLE LOCKING MECHANISM WITH ACCESSIBLE EXTERNAL COUPLING
US5016931A (en) * 1989-06-20 1991-05-21 The Hartwell Corporation Latching mechanism having a pre-adjusted load
US5234238A (en) * 1991-09-26 1993-08-10 Takigen Manufacturing Co., Ltd. Ratchet type latch assembly
US5595409A (en) * 1994-07-05 1997-01-21 Anderson Corporation Gliding door latch assembly
US5802892A (en) * 1996-05-08 1998-09-08 Metro Industries, Inc. Storage system including multifunction lock assembly utilizing lock latch mechanism and lock latch extension mechanism
EP0839714B2 (en) 1996-10-30 2016-07-06 The Boeing Company Double stroke over center latch
US6036238A (en) * 1996-10-30 2000-03-14 The Boeing Company Double stroke over center latch
US6234426B1 (en) * 1998-12-03 2001-05-22 Trw Inc. Modular spacecraft construction requiring no tools for assembly and disassembly
WO2002016717A1 (en) * 2000-08-22 2002-02-28 Huf Hülsbeck & Fürst Gmbh & Co. Kg Distance-variable closing stirrup for rotary-latch locks
US6722717B2 (en) 2000-08-22 2004-04-20 Huf Hülsbeck & Fürst Gmbh & Co. Kg Distance-variable closing stirrup for rotary-latch locks
US6755448B2 (en) 2001-06-20 2004-06-29 Hartwell Corporation Blowout latch
US7097219B2 (en) * 2002-05-03 2006-08-29 Anchor Tool & Die Company Encapsulated striker assembly
US20030205904A1 (en) * 2002-05-03 2003-11-06 Paskonis Almantas K. Encapsulated striker assembly
US7111881B2 (en) 2002-12-19 2006-09-26 Tinnerman Palnut Engineered Products, Inc. Single-piece latch strikers with mechanically locked components
US20050167993A1 (en) * 2002-12-19 2005-08-04 Paskonis Almantas K. Single-piece latch strikers with mechanically locked components
US20050218671A1 (en) * 2004-04-06 2005-10-06 Honda Motor Co., Ltd. Structure for attaching striker, having attachment bracket including base and protruding portion
US7222893B2 (en) * 2004-04-06 2007-05-29 Honda Motor Co., Ltd. Structure for attaching striker, having attachment bracket including base and protruding portion
US20060214431A1 (en) * 2005-03-25 2006-09-28 Helsley Thomas J Latch mechanism
US7185926B2 (en) 2005-03-25 2007-03-06 Hartwell Corporation Preloaded latch mechanism
US20070241570A1 (en) * 2006-04-03 2007-10-18 Paskonis Almantas K Latch and latch striker interface improvements
US20100051748A1 (en) * 2008-08-26 2010-03-04 Etling Keith A Flush-mounted latching assembly and method of assembling same
US8201856B2 (en) 2008-08-26 2012-06-19 The Boeing Company Flush-mounted latching assembly
US20110133489A1 (en) * 2009-12-09 2011-06-09 Airbus Operations Sas Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
US8894012B2 (en) * 2009-12-09 2014-11-25 Airbus Operations Sas Aircraft nacelle incorporating a hood closure device that is independent of the locking mechanism
US8864185B2 (en) * 2010-03-18 2014-10-21 Alcoa Inc. Latch with adjustable handle
US20110227350A1 (en) * 2010-03-18 2011-09-22 Thai Do Latch with adjustable handle
CN102971213A (en) * 2010-07-09 2013-03-13 空中客车运营简化股份公司 Method for adjusting the doors of a landing gear bay, and associated door
CN102971213B (en) * 2010-07-09 2016-04-13 空中客车运营简化股份公司 The control method of alighting gear frame cabin door and the hatch door of enforcement
US9376215B2 (en) 2013-01-29 2016-06-28 United Technologies Corporation Cowl with pressure driven latch
US9845708B2 (en) 2013-01-29 2017-12-19 United Technologies Corporation Cowl with rate limited lock
US9273488B1 (en) * 2013-07-15 2016-03-01 Avibank Manufacturing, Inc. Positive locking keeper
US11041331B2 (en) 2015-04-03 2021-06-22 Howmet Aerospace Inc. Latch having tool recess in trigger
US10337218B2 (en) 2015-07-08 2019-07-02 Arconic Inc. Handle mechanisms
US10604977B2 (en) 2015-08-04 2020-03-31 Arconic Inc. Pressure relief latch
US10435929B2 (en) 2015-08-26 2019-10-08 Arconic Inc. Adjustable pressure relief latch
US10760304B2 (en) 2015-09-01 2020-09-01 Howmet Aerospace Inc. Adjustable hook latch
US10240389B2 (en) 2015-09-30 2019-03-26 Arconic Inc. Pressure relief door
US10378256B2 (en) 2015-10-30 2019-08-13 Arconic Inc. Pressure relief latch
US10309126B2 (en) 2016-01-21 2019-06-04 Arconic Inc. Pawl latch
US10676971B2 (en) 2016-06-13 2020-06-09 Arconic Inc. Rotary latch system
CN110319325A (en) * 2019-04-03 2019-10-11 广州文冲船厂有限责任公司 A kind of cabinet mounting structure
US20220267018A1 (en) * 2021-02-20 2022-08-25 Andres Hernandez High visibility hook latch

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